02654nam 2200649Ia 450 991070035820332120110613151129.0(CKB)5470000002409404(OCoLC)730263676(EXLCZ)99547000000240940420110613d2010 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierLoop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds[electronic resource] /Joseph W. Connolly and George Kopasakis ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010Cleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2010]1 online resource (19 pages) illustrations (color)NASA/TM ;2010-216897Title from title screen (viewed on June 13, 2011)."October 2010.""AIAA-2010-7068."Includes bibliographical references (pages 18-19).Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory Supersonic flightnasatControl systems designnasatSupersonic transportsnasatSpecificationsnasatSupersonic inletsnasatDynamic modelsnasatLoopsnasatFeedback controlnasatSupersonic wind tunnelsnasatFlow distributionnasatComputational fluid dynamicsnasatSupersonic flight.Control systems design.Supersonic transports.Specifications.Supersonic inlets.Dynamic models.Loops.Feedback control.Supersonic wind tunnels.Flow distribution.Computational fluid dynamics.Connolly Joseph W1398989Kopasakis George1395866NASA Glenn Research Center.AIAA/ASME/SAE/ASEE Joint Propulsion Conference(46th :2010 :Nashville, Tenn.)GPOGPOBOOK9910700358203321Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds3463398UNINA